fgbuoyantforces.h

来自「6 DOF Missle Simulation」· C头文件 代码 · 共 181 行

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%

 Header:       FGBuoyantForces.h
 Author:       Anders Gidenstam, Jon S. Berndt
 Date started: 01/21/08

 ------------- Copyright (C) 2008  Anders Gidenstam               -------------
 ------------- Copyright (C) 2008  Jon S. Berndt ([e-mail]) -------------

 This program is free software; you can redistribute it and/or modify it under
 the terms of the GNU Lesser General Public License as published by the Free Software
 Foundation; either version 2 of the License, or (at your option) any later
 version.

 This program is distributed in the hope that it will be useful, but WITHOUT
 ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
 FOR A PARTICULAR PURPOSE.  See the GNU Lesser General Public License for more
 details.

 You should have received a copy of the GNU Lesser General Public License along with
 this program; if not, write to the Free Software Foundation, Inc., 59 Temple
 Place - Suite 330, Boston, MA  02111-1307, USA.

 Further information about the GNU Lesser General Public License can also be found on
 the world wide web at http://www.gnu.org.

HISTORY
--------------------------------------------------------------------------------
01/21/08   JSB   Created

%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
SENTRY
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#ifndef FGBuoyanTFORCES_H
#define FGBuoyanTFORCES_H

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
INCLUDES
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

#include <vector>
#include <map>

#include "FGModel.h"
#include "FGGasCell.h"
#include <math/FGColumnVector3.h>
#include <input_output/FGXMLFileRead.h>

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
DEFINITIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

#define ID_BUOYANTFORCES "$Id$"

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
FORWARD DECLARATIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

namespace JSBSim {

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CLASS DOCUMENTATION
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

/** Encapsulates the Buoyant forces calculations.
    This class owns and contains the list of force/coefficients that define the
    Buoyant properties of an air vehicle.
    
    Here's an example of a gas cell specification:

    @code
    <buoyant_forces>
      <gas_cell type="HYDROGEN">
        <location unit="M">
          <x> 18.8 </x>
          <y> 0.0 </y>
          <z> 0.0 </z>
        </location>
        <x_radius unit="M"> 22.86 </x_radius>
        <y_radius unit="M">  4.55 </y_radius>
        <z_radius unit="M">  4.55 </z_radius>
        <max_overpressure unit="PA"> 340.0 </max_overpressure> 
        <valve_coefficient unit="M4*SEC/KG"> 0.015 </valve_coefficient>
      </gas_cell>
      
      ... {other gass cells} ...
      
    </buoyant_forces>
    @endcode

    See FGGasCell for the full configuration file format for gas cells.

    @author Anders Gidenstam, Jon S. Berndt
    @version $Id$
*/

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CLASS DECLARATION
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

class FGBuoyantForces : public FGModel, public FGXMLFileRead
{

public:
  /** Constructor
      @param Executive a pointer to the parent executive object */
  FGBuoyantForces(FGFDMExec* Executive);
  /// Destructor
  ~FGBuoyantForces();

  bool InitModel(void);

  /** Runs the Buoyant forces model; called by the Executive
      @return false if no error */
  bool Run(void);

  /** Loads the Buoyant forces model.
      The Load function for this class expects the XML parser to
      have found the Buoyant_forces keyword in the configuration file.
      @param element pointer to the current XML element for Buoyant forces parameters.
      @return true if successful */
  bool Load(Element* element);

  /** Gets the total Buoyant force vector.
      @return a force vector. */
  FGColumnVector3 GetForces(void) {return vTotalForces;}

  /** Gets the total Buoyancy moment vector.
      @return a moment vector. */
  FGColumnVector3 GetMoments(void) {return vTotalMoments;}

  /** Gets the total gas mass. The gas mass is part of the aircraft's
      inertia.
      @return mass in slugs. */
  double GetGasMass(void);

  /** Gets the total moment from the gas mass.
      @return a moment vector. */
  FGColumnVector3& GetGasMassMoment(void);

  /** Gets the total moments of inertia for the gas mass.
      @return . */
  FGMatrix33& GetGasMassInertia(void);

  /** Gets the strings for the current set of gas cells.
      @param delimeter either a tab or comma string depending on output type
      @return a string containing the descriptive names for all parameters */
  string GetBuoyancyStrings(string delimeter);

  /** Gets the coefficient values.
      @param delimeter either a tab or comma string depending on output type
      @return a string containing the numeric values for the current set of
      parameters */
  string GetBuoyancyValues(string delimeter);

private:
  vector <FGGasCell*> Cells;
  // Buoyant forces and moments. Excluding the gas weight.
  FGColumnVector3 vTotalForces;
  FGColumnVector3 vTotalMoments;

  // Gas mass related masses, inertias and moments.
  FGMatrix33 gasCellJ;
  FGColumnVector3 vGasCellXYZ;
  FGColumnVector3 vXYZgasCell_arm;

  bool NoneDefined;

  void bind(void);
  void unbind(void);

  void Debug(int from);
};

} // namespace JSBSim

//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
#endif